Multi-rotor UAV with detachable dual-propeller structure
A multi-rotor UAV, detachable technology, applied in the field of UAV, can solve the problem of low flight efficiency of multi-rotor UAV, and achieve the effect of high flight efficiency
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[0040] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art belong to the scope of protection of the present invention; among them, the "and / or" keyword involved in the present embodiment means and, or both In other words, A and / or B mentioned in the embodiments of the present invention represent two situations of A and B, A or B, and describe the three states of A and B, such as A and / or B means: only include A but not B; only include B but not A; include A and B.
[0041] At the same time, in the embodiments of the present invention, when a component is referred to as being "fixed"...
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